Key statistics
Satellite SL-16 DEB at a glance.
Uptime
10902
Days in orbit
Revolutions
≈ 13.7
Per day
Orbit
LEO
Low Earth Orbit
Inclination
71.0
Latest
Satellite identification and parameters
Extended collection of information and parameters for SL-16 DEB.
Object identification
Identified? True
Debris? True
Object name: SL-16 DEB
International designator: 1995-058D
Object number (NORAD): 23707
Object ID (CCSDS): 23707
Country: COMMONWEALTH OF INDEPENDENT STATES (CIS)
Current information (Y/N): Y
RCS size: SMALL
Orbital parameters
Period: 104.922 minutes
Inclination: 70.9975 deg
SMA: 7368.95 km
Apoapsis: 1141.538 km
Periapsis: 840.093 km
RAAN: 335.1574 deg
Eccentricy: 0.02045371
Argument of periapsis: 166.0419 deg
Mean anomaly: 218.9718 deg
Mean motion: 13.72442961 rev/day
Mean motion (dot): 0.00000163 rev/day2
B* drag term: 0.00019278028 1/REarth
Two-line elements (TLE)
Creation date: Sept. 3, 2025, 10:15 a.m.
Reference frame: TEME
Reference center: EARTH
Epoch: Sept. 3, 2025, 6:54 a.m. UTC
TLE line 0: 0 SL-16 DEB
TLE line 1: 1 23707U 95058D 25246.28813670 .00000163 00000-0 19278-3 0 9990
TLE line 2: 2 23707 70.9975 335.1574 0204537 166.0419 218.9718 13.72442961494006
Live tracking on map
Real-time ground track for satellite SL-16 DEB.
Associated space launch
Second generation ELING satellite
SL-16 DEB was lifted into orbit during the mission ‘Zenit-2 | Tselina-2 17’, on board a Zenit-2 space rocket.
The launch took place on Oct. 31, 1995, 8:19 p.m. from 45/1.
For more information about the launch, click the button.
Zenit-2 | Tselina-2 17
Agency: N/A
Status: Launch Successful
Launch date: Oct. 31, 1995, 8:19 p.m. UTC
Rocket: Zenit-2
Launch pad: 45/1
Location: Baikonur Cosmodrome, Republic of Kazakhstan
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